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¡ß Project
Overview
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Project
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Development
of Very Small Turboshaft for UAV
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Schedule :
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September,
2001 ~ January, 2006
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Sponsor
&
Supervisor:
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Ministry of
Commerce, Industry and Energy
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Leading
Company:
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Neuros Co.,
Ltd.
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Participating
Institues :
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Korea Aerospace
Research Institute, Korea Institute
of Machinery & Materials
Seoul
National University,
SeJong University
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¡ß Development
Goal
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Development of world class very small
turboshaft engine for UAV
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- Development
of turbojet engine with the same engine
core
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¡ß Specifications
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Shaft Horse Power
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65 shp @ S.L.S.
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Compressor
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Radial Compressor (single
stage)
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Gas Generator Turbine
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Axial Turbine (single
stage)
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Free Power Turbine
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Axial Turbine (single
stage)
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R.P.M.
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105,000
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Dimension
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550 mm (L) × 150
mm (D)
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Specific Fuel Consumption
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0.95 lb/h/shp @
S.L.S.
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Weight
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¡Â 15 kg (including
gearbox)
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Turboshaft
Engine under Development
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¡ß Potential
Applications
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Unmanned helicopters used in traffic
monitoring, aerial photography, etc.
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- Auxiliary
Power Unit (APU)
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¡ß Features
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High Power Density : 4.3 shp/kg
weight
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- Wide Operating
Range : Sea level ~ 15,000 ft
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- Digital Electronic
Engine Control
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- Long Life
: 1,000 h
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¡ß Specifications
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Thrust
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55 lbf @ S.L.S.
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Compressor
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Radial Compressor (single
stage)
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Gas Generator Turbine
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Axial Turbine (single
stage)
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Free Power Turbine
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Axial Turbine (single
stage)
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R.P.M.
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105,000
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Dimension
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350 mm (L) × 150
mm (D)
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Specific Fuel Consumption
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1.2 lb/h/lb @
S.L.S.
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Weight
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¡Â 10 kg
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Turbojet
Engine under Development
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¡ß Potential
Applications
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-
Unmanned aircraft used in traffic
monitoring, aerial photography, etc.
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- Unmanned
Aerial Vehicle
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¡ß Features
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High Thrust-to-Weight Ratio: 6.0 lbf/kg
weight
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- Wide Operating
Range : Sea level ~ 35,000 ft
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- Digital Electronic
Engine Control
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- Long Life
: 1,000 h
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